Aerodynamic Design of Integrated Propulsion-Airframe Configuration of the Hybrid Wing-Body AircraftHybrid Wing Body (HWB) aircraft is characterized by a flattened and airfoil-shaped body, which produces a substantial portion of the total lift. The body form is composed of distinct and separate wing structures, though the wings are smoothly blended into the body. This concept has been studied widely and results suggest remarkable performance improvements over the conventional tube and wing transport1,2. HWB incorporates design features from both a futuristic fuselage and flying wing design, which houses most of the crew, payload and equipment inside the main centerbody structure.
Document ID
20170008006
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Liou, May-Fun (NASA Glenn Research Center Cleveland, OH United States)
Kim, Hyoungjin (Science Applications International Corp. Beavercreek, OH, United States)
Lee, B. J. (Vantage Partners, LLC Cleveland, OH, United States)
Liou, Meng-Sing (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
August 28, 2017
Publication Date
June 8, 2017
Subject Category
AerodynamicsAircraft Design, Testing And Performance
Report/Patent Number
GRC-E-DAA-TN43199
Meeting Information
Meeting: AIAA Aviation 2017
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics